View from above orbital plane
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View from above satellite
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Ground track
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The orbit is defined by the following mean orbital elements,
1 26474U 26066.97383589 +.00000000 +00000-0 +41714-3 0 00008
2 26474 67.9897 45.3349 0038446 37.4461 322.9355 15.09542594 02
| Epoch (UTC): | 07 March 2026 23:22:19 |
| Eccentricity: | 0.0038446 |
| inclination: | 67.9897° |
| perigee height: | 511 km |
| apogee height: | 564 km |
| right ascension of ascending node: | 45.3349° |
| argument of perigee: | 37.4461° |
| revolutions per day: | 15.09542594 |
| mean anomaly at epoch: | 322.9355° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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